groovyBC and probe problem, needing your help!
I am simulating the synthetic jet on NACA 0015 airfoil.
so I have a suction/blowing type boundary condition, and a prescribed velocity distribution is imposed at the boundary:
y=47.95*sin(2*pi*50*time). It's normal to the patch.
I have a groobyBC type boundary condition in my ./0/U, the code is
Any hints very much appreciated!
Then look at the result in paraview (cell values!!!!).
- a problem with the other boundary conditions
- an interpolation problem
For all these I deny all responsibility
Does the vector normal() generally have the length 1 ?
For a test I would replace normal() with normal() / mag(normal()) .
Thanks for your all quick reply!
I'll have try!
I'll post the result as soon as i get it.
I think you are right!
With the utility of patchAverage, I found the magnititude of velocity is right now. Although the point (0.045 0.02338 0.01875) is near the patch, the velocity is not right of the jet patch with the effect of other patch.
It's not the groovy and probes problem.
Now everything is going well!
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